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SiC Fiber Reinforced Ceramic Matrix Composites for Turbine Engine Applications

[+] Author Affiliations
Kenneth Hatton, Dennis Landini, Stan Hemstad

Honeywell Advanced Composites Inc., Newark, DE

R. Craig Robinson

Dynacs Aerospace Company, Inc., Brook Park, OH

Paper No. 2000-GT-0072, pp. V004T02A010; 4 pages
  • ASME Turbo Expo 2000: Power for Land, Sea, and Air
  • Volume 4: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education
  • Munich, Germany, May 8–11, 2000
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7857-6
  • Copyright © 2000 by ASME


Honeywell Advanced Composites Inc. (ACI) has been working with OEM’s to develop, fabricate, and test ceramic matrix composite (CMC) materials for partial and full replacement of hot section turbine engine components. Using Chemical Vapor Infiltration (CVI) technology, silicon carbide fiber reinforced silicon carbide matrix parts, such as full annular combustion liners and inserts for leading edges on nozzle guide vanes have been fabricated and tested.

Copyright © 2000 by ASME



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